242450 2004QY2 help
Last update: 2025-09-10 00:30 UTC
Epoch
Orbit properties
  • Epoch
  • Semimajor Axis
  • Eccentricity (e)
  • Inclination (i)
  • Long. of Ascending Node (Ω)
  • Arg. of Perihelion (ω)
  • Mean Anomaly (M)
  • Perihelion distance
  • Aphelion distance
  • Asc. Node-Earth Sep.
  • Desc. Node-Earth Sep.
  • MOID
  • Orbit Period
  • U parameter
Value
1-sigma variation
Unit
Epoch
Value
61000.0000
1-sigma variation
Unit
MJD
Semimajor Axis
Value
1.083864
1-sigma variation
2.674E-9
Unit
Eccentricity (e)
Value
0.477121
1-sigma variation
3.597E-8
Unit
-
Inclination (i)
Value
37.0332
1-sigma variation
6.923E-6
Unit
Long. of Ascending Node (Ω)
Value
295.2719
1-sigma variation
7.210E-6
Unit
Arg. of Perihelion (ω)
Value
104.9856
1-sigma variation
8.266E-6
Unit
Mean Anomaly (M)
Value
224.10799
1-sigma variation
0.00001
Unit
Perihelion distance
Value
0.566730
1-sigma variation
Unit
Aphelion distance
Value
1.600999
1-sigma variation
Unit
Asc. Node-Earth Sep.
Value
-0.062730
1-sigma variation
Unit
Desc. Node-Earth Sep.
Value
-0.238822
1-sigma variation
Unit
MOID
Value
0.047899
1-sigma variation
Unit
Orbit Period
Value
412.1553
1-sigma variation
Unit
U parameter
Value
0.0
1-sigma variation
Unit
-
Covariance Matrix
aeiΩωM
a7.15013E-189.82531E-182.98545E-162.07310E-15-1.43360E-15-1.66832E-14
e9.82531E-181.29367E-154.29821E-146.62138E-14-6.89357E-149.99056E-14
i2.98545E-164.29821E-144.79297E-11-3.38163E-13-2.20095E-125.71459E-12
Ω2.07310E-156.62138E-14-3.38163E-135.19842E-11-3.47986E-11-2.01869E-11
ω-1.43360E-15-6.89357E-14-2.20095E-12-3.47986E-116.83238E-11-2.16511E-11
M-1.66832E-149.99056E-145.71459E-12-2.01869E-11-2.16511E-118.38160E-11
Date of computation: 2025-09-10 00:30 UTC
Note: The ASCII file is in a format suitable for Orbfit input.
Download ASCII file: